Abstract
The influence of centerline and the cross-section variation to aerodynamic performance of the inlet was researched in a wider range. A new method of measuring the total pressure recovery coefficient and total pressure distortion coefficient of the inlet was proposed. Based on the loitering aircraft, a s-shaped inlet was designed to meet the needs of stable flight of loitering aircraft, whose total pressure recovery coefficient is 93.2% and total pressure distortion coefficient is 1.2%.
| Original language | English |
|---|---|
| Title of host publication | Materials Processing Technology |
| Pages | 349-354 |
| Number of pages | 6 |
| DOIs | |
| Publication status | Published - 2011 |
| Event | 2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011 - Sanya, China Duration: 29 Jul 2011 → 31 Jul 2011 |
Publication series
| Name | Advanced Materials Research |
|---|---|
| Volume | 291-294 |
| ISSN (Print) | 1022-6680 |
Conference
| Conference | 2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011 |
|---|---|
| Country/Territory | China |
| City | Sanya |
| Period | 29/07/11 → 31/07/11 |
Keywords
- Distortion coefficient
- Loitering aircraft
- Recovery coefficient
- S-shaped inlet
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He, G., & Li, X. (2011). Design of s-shaped submerged inlet. In Materials Processing Technology (pp. 349-354). (Advanced Materials Research; Vol. 291-294). https://doi.org/10.4028/www.scientific.net/AMR.291-294.349